Aerothermodynamic Performance Analysis of Hypersonic Flow on Power Law Leading Edges

2005 ◽  
Vol 42 (4) ◽  
pp. 588-597 ◽  
Author(s):  
Wilson F. N. Santos ◽  
Mark J. Lewis
Keyword(s):  
Performance Analysis ◽  
Hypersonic Flow ◽  
Power Law ◽  
Leading Edges

Power-Law Shaped Leading Edges in Rarefied Hypersonic Flow

2002 ◽  
Vol 39 (6) ◽  
pp. 917-925 ◽  
Author(s):  
Wilson F. N. Santos ◽  
Mark J. Lewis
Keyword(s):  
Hypersonic Flow ◽  
Power Law ◽  
Leading Edges

Axisymmetric hypersonic flow with strong viscous interaction

1968 ◽  
Vol 34 (4) ◽  
pp. 687-703 ◽  
Author(s):  
John Webster Ellinwood ◽  
Harold Mirels
Keyword(s):  
Shock Wave ◽  
Hypersonic Flow ◽  
Power Law ◽  
Axisymmetric Flow ◽  
Strong Shock ◽  
The Body ◽  
Strong Shock Wave ◽  
Viscous Interaction ◽  
Slender Bodies ◽  
Prandtl Numbers

Stewartson's theory for axisymmetric hypersonic flow of a model gas over slender bodies with strong viscous interaction and strong shock wave is extended to power-law viscosity variation and Prandtl numbers other than one. Flow properties at the body surface and shock are obtained without recourse to numerical integration. Numerical computations are presented for axisymmetric flow over a three-quarter power-law body with strong shock wave and viscous interactions that range from weak to strong.

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